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公开(公告)号：WO2012090071A2
公开(公告)日：2012-07-05
申请号：PCT/IB2011/003329
申请日：2011-12-30
Applicant: ROYCE POWER ENGINEERING PLC , INNES, MAtthew, Christopher , WHENHAM, Ian , COURBARIAUX, Yann , BOHAN, Margaret, Kathleen
Inventor： INNES, MAtthew, Christopher , WHENHAM, Ian , COURBARIAUX, Yann , BOHAN, Margaret, Kathleen
CPC classification number: F02C7/222 , B05B7/02 , F02C7/22 , F23D11/38 , F23D14/02 , F23D17/002 , F23R3/30 , F23R3/36
Abstract: A system includes a turbine engine having a fuel injector. The fuel injector includes fluid ducts, each having a fuel inlet coupled to a distinct fuel source. The system includes a compressed air source that provides compressed air simultaneously to the fluid ducts, and a convergence point where combined fuel and air streams from the ducts are mixed. The fuel inlets are in a parallel flow arrangement such that no fuel from one fuel injector is present at another fuel injector.
Abstract translation: 一种系统包括具有燃料喷射器的涡轮发动机。 燃料喷射器包括流体管道，每个流体管道具有联接到不同燃料源的燃料入口。 该系统包括将压缩空气同时提供给流体管道的压缩空气源，以及来自管道的组合的燃料和空气流混合的会聚点。 燃料入口是平行的流动布置，使得在另一个燃料喷射器处不存在来自一个燃料喷射器的燃料。
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2.发明申请MULTI-FUEL INJECTOR HAVING SEPERATE AIR - PREMIXING STRUCTURES FOR THE PLURALITY OF FUELS AND A CONSEQUENT COMMON MIXING STRUCTURE BEFORE THE NOZZLE OUTLET 审中-公开具有空气燃料的多燃料喷射器 - 燃料多余的先进结构和在喷嘴出口之前的相应的常见混合结构
公开(公告)号：WO2012090071A3
公开(公告)日：2012-08-23
申请号：PCT/IB2011003329
申请日：2011-12-30
Applicant: ROYCE POWER ENGINEERING PLC , INNES MATTHEW CHRISTOPHER , WHENHAM IAN , COURBARIAUX YANN , BOHAN MARGARET KATHLEEN
Inventor： INNES MATTHEW CHRISTOPHER , WHENHAM IAN , COURBARIAUX YANN , BOHAN MARGARET KATHLEEN
CPC classification number: F02C7/222 , B05B7/02 , F02C7/22 , F23D11/38 , F23D14/02 , F23D17/002 , F23R3/30 , F23R3/36
Abstract: A system includes a turbine engine having a fuel injector (100). The fuel injector (100) includes fluid ducts (103,105,107), each having a fuel inlet (108,110,212) coupled to a distinct fuel source. The system includes a compressed air source that provides compressed air simultaneously to the fluid ducts (103,105,107), and a convergence point (106) where combined fuel and air streams from the ducts are mixed. The fuel inlets (108,110, 112) are in a parallel flow arrangement such that no fuel from one fuel inlet (108,110,212) is present at another fuel inlet (108,110,212)
Abstract translation: 一种系统包括具有燃料喷射器（100）的涡轮发动机。 燃料喷射器（100）包括流体管道（103,105,107），每个流体管道具有联接到不同燃料源的燃料入口（108,110,212）。 该系统包括压缩空气源，其同时向流体管道（103,105,107）提供压缩空气，以及汇合点（106），其中来自管道的组合的燃料和空气流混合。 燃料入口（108,110,112）是平行的流动布置，使得在另一个燃料入口（108,110,212）处不存在来自一个燃料入口（108,110,212）的燃料，
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3.发明申请MULTI-FUEL INJECTOR HAVING SEPERATE AIR - PREMIXING STRUCTURES FOR THE PLURALITY OF FUELS AND A CONSEQUENT COMMON MIXING STRUCTURE BEFORE THE NOZZLE OUTLET 审中-公开具有空气燃料的多燃料喷射器 - 燃料多余的先进结构和在喷嘴出口之前的相应的常见混合结构
公开(公告)号：WO2012090071A8
公开(公告)日：2014-01-03
申请号：PCT/IB2011003329
申请日：2011-12-30
Applicant: ROLLS ROYCE POWER ENG , INNES MATTHEW CHRISTOPHER , WHENHAM IAN , COURBARIAUX YANN , BOHAN MARGARET KATHLEEN
Inventor： INNES MATTHEW CHRISTOPHER , WHENHAM IAN , COURBARIAUX YANN , BOHAN MARGARET KATHLEEN
CPC classification number: F02C7/222 , B05B7/02 , F02C7/22 , F23D11/38 , F23D14/02 , F23D17/002 , F23R3/30 , F23R3/36
Abstract: A system includes a turbine engine having a fuel injector (100). The fuel injector (100) includes fluid ducts (103,105,107), each having a fuel inlet (108,110,212) coupled to a distinct fuel source. The system includes a compressed air source that provides compressed air simultaneously to the fluid ducts (103,105,107), and a convergence point (106) where combined fuel and air streams from the ducts are mixed. The fuel inlets (108,110, 112) are in a parallel flow arrangement such that no fuel from one fuel inlet (108,110,212) is present at another fuel inlet (108,110,212)
Abstract translation: 一种系统包括具有燃料喷射器（100）的涡轮发动机。 燃料喷射器（100）包括流体管道（103,105,107），每个流体管道具有联接到不同燃料源的燃料入口（108,110,212）。 该系统包括压缩空气源，其同时向流体管道（103,105,107）提供压缩空气，以及汇合点（106），其中来自管道的组合的燃料和空气流混合。 燃料入口（108,110,112）是平行的流动布置，使得在另一个燃料入口（108,110,212）处不存在来自一个燃料入口（108,110,212）的燃料，
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